Machine Design: cram pack

Formula sheets, the key method steps for every topic and 12 practice problems, with full solutions at the back.

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1Formulas and methods

Gears & gear trains

Meshing gears
n1·N1 = n2·N2
Torque
T2 = T1·(N2/N1)·η
Power
P = T·ω, ω = 2π·n/60
Compound train
total ratio = product of the stage ratios

Torsion of shafts

Shear stress
τ = T·r/J
Solid shaft
J = πd⁴/32
Hollow shaft
J = π(D⁴ − d⁴)/32
Angle of twist
φ = TL/(GJ)
Power
P = T·ω = 2πnT/60

Method

  1. Find the polar moment of area: J = πd⁴/32 for a solid shaft.
  2. Shear stress at the surface: τ = T·r/J, with r the outer radius.
  3. Angle of twist: φ = TL/(GJ) in radians.
  4. If power is given, find the torque first with P = T·ω, ω = 2πn/60.

Mohr’s circle & stress transformation

Centre
C = (σx + σy)/2
Radius
R = √(((σx − σy)/2)² + τxy²)
Principal stresses
σ1,2 = C ± R
Principal direction
tan 2θp = 2τxy/(σx − σy)
Inclined plane
σθ = C + (σx − σy)/2·cos 2θ + τxy·sin 2θ

Method

  1. Calculate the centre of Mohr’s circle: C = (σx + σy)/2.
  2. Calculate the radius: R = √(((σx − σy)/2)² + τxy²).
  3. The principal stresses are C ± R and the largest in-plane shear stress is R.
  4. Angles on the circle are double the angles on the element: tan 2θp = 2τxy/(σx − σy).

Axial stress & strain

Normal stress
σ = F/A
Strain
ε = ΔL/L
Hooke’s law
σ = E·ε
Elongation
ΔL = FL/(EA)
Thermal strain
εT = α·ΔT

Column buckling

Euler load
Pcr = π²EI/(KL)²
Effective length factor
K = 1 pinned–pinned, 0.5 fixed–fixed, 0.7 fixed–pinned, 2 fixed–free
Critical stress
σcr = Pcr/A
Slenderness
λ = KL/r, r = √(I/A)

Mechanical vibrations

Natural frequency
ωn = √(k/m), fn = ωn/(2π)
From static deflection
ωn = √(g/δst)
Critical damping
cc = 2√(km) = 2mωn
Damping ratio
ζ = c/cc
Damped frequency
ωd = ωn√(1 − ζ²)
Logarithmic decrement
δ = (1/n)·ln(x0/xn), ζ = δ/√(4π² + δ²)
Springs in parallel
k = k1 + k2
Springs in series
1/k = 1/k1 + 1/k2

2Practice problems

1.Gears & gear trainsMedium
d1​ = 80 mmd2​ = 315 mm960 rpmT1​ = 500 NT2​ = 250 NP = ?

A belt runs on an 80 mm driving pulley at 960 rpm. The tension is 500 N on the tight side and 250 N on the slack side. Find the power P transmitted, in kW.

d1 = 80 mmn1 = 960 rpmT1 = 500 NT2 = 250 N
P = kW
2.Gears & gear trainsHard
d1​ = 125 mmd2​ = 250 mm1450 rpmC = 600 mmT1​ = 1200 NT2​P = ?

An open belt connects a 125 mm driving pulley at 1450 rpm to a 250 mm pulley; the centres are 600 mm apart. The coefficient of friction is 0.25 and the tight-side tension may not exceed 1200 N. Find the largest power P the belt can transmit without slipping, in kW (ignore centrifugal effects).

d1 = 125 mmn1 = 1450 rpmd2 = 250 mmC = 600 mmμ = 0.25T1 = 1200 N
P = kW
3.Torsion of shaftsMedium
d1​ = 25 mmd2​ = 20 mmT = 100 N·mABC1.2 m1.2 m

A stepped solid steel shaft is fixed at A. Segment AB has diameter 25 mm and length 1.2 m; segment BC has diameter 20 mm and length 1.2 m. A torque of 100 N·m acts at the free end C. Find the maximum shear stress τmax in the shaft.

T = 100 N·md1 = 25 mm, L1 = 1.2 md2 = 20 mm, L2 = 1.2 m
τmax = MPa
4.Torsion of shaftsHard
d = 20 mmTB​ = 200 N·mTC​ = 100 N·mABC1.5 m2.5 m

A solid aluminium shaft of diameter 20 mm is fixed at A. A torque of 200 N·m acts at B, 1.5 m from A, and a torque of 100 N·m in the same direction acts at the free end C, a further 2.5 m along. Find the maximum shear stress τmax in the shaft.

d = 20 mmTB = 200 N·mTC = 100 N·mAB = 1.5 mBC = 2.5 m
τmax = MPa
5.Mohr’s circle & stress transformationMedium
σx​ = 80σy​ = 70τxy​ = 20MPa

A point in a loaded part has σₓ = 80 MPa, σᵧ = 70 MPa and τₓᵧ = 20 MPa (tension positive). Find the angle θp from the x-axis to the direction of the largest principal stress, between −90° and 90°.

σx = 80 MPaσy = 70 MPaτxy = 20 MPa
θp = °
6.Mohr’s circle & stress transformationHard
σx​ = 150σy​ = −70τxy​ = −50MPa

A point in a loaded part has σₓ = 150 MPa, σᵧ = −70 MPa and τₓᵧ = −50 MPa (tension positive). Find the normal stress σθ on a plane whose normal is rotated 35° counter-clockwise from the x-axis.

σx = 150 MPaσy = −70 MPaτxy = −50 MPaθ = 35°
σθ = MPa
7.Axial stress & strainMedium
Ø 10 mmAluminium1.5 mP = 90 kN

Find the elongation δ of the aluminium bar under the axial load.

P = 90 kNd = 10 mmL = 1.5 mE = 70 GPa
δ = mm
8.Axial stress & strainHard
60 kN12400 mm200 mmØ25Ø40σ2​ = ?

A steel segment (diameter 25 mm, length 400 mm, E = 200 GPa) and a segment made of brass (diameter 40 mm, length 200 mm, E = 100 GPa) are joined end to end and fixed between two rigid walls. An axial load of 60 kN acts at the joint, towards segment 2. Find the magnitude of the stress σ2 in segment 2.

segment 1: steel, Ø25 mm, 400 mm, E = 200 GPasegment 2: brass, Ø40 mm, 200 mm, E = 100 GPaP = 60 kN
σ2 = MPa
9.Column bucklingMedium
PL = 3 md = 50 mmcross-section

A column of length L made of aluminium is fixed at the base and free at the top. Using Euler’s formula, find its critical buckling load Pcr.

L = 3 mE = 70 GPa (aluminium)d = 50 mm
Pcr = kN
10.Column bucklingHard
P = 85 kNL = 4 md = ?cross-section

A solid round column of length L made of aluminium is fixed at both ends. It must carry 85 kN with a factor of safety of 3 against buckling. Find the smallest diameter d.

P = 85 kNn = 3L = 4 mE = 70 GPa (aluminium)
d = mm
11.Mechanical vibrationsMedium
tx10 mm2 cycles4.7 mm

In a free-vibration test of a damped mass–spring system, a displacement peak of 10 mm is followed 2 cycles later by a peak of 4.7 mm. Find the damping ratio ζ.

x0 = 10 mmx2 = 4.7 mmn = 2
ζ =
12.Mechanical vibrationsHard
k1​ = 12k2​ = 12k3​ = 20m = 10 kg

A 10 kg mass hangs from spring k₃ = 20 kN/m. The top of k₃ is attached to a rigid bar that hangs from two springs side by side, k₁ = 12 kN/m and k₂ = 12 kN/m; the bar stays level. Ignore damping and the masses of the springs and bar. Find the natural frequency fn of vertical vibration in Hz.

m = 10 kgk1 = 12 kN/mk2 = 12 kN/mk3 = 20 kN/m
fn = Hz

3Solutions

1.Gears & gear trains

Answer: P = 1.005 kW

Belt drives: without slip, both pulleys have the same rim speed v = π·d·n/60, so n₁·d₁ = n₂·d₂ and the speed ratio is d₂/d₁. Slip s makes the driven pulley a little slower: n₂ = n₁·(d₁/d₂)·(1 − s). The power transmitted is P = (T₁ − T₂)·v, with T₁ the tension on the tight side and T₂ on the slack side. Friction limits the ratio of the tensions: T₁/T₂ = eμθ, where θ is the angle of wrap in radians on the smaller pulley; for an open belt θ = π − 2·asin((d₂ − d₁)/(2C)) with centre distance C.

Belt speed

v = 4.021 m/s

Power

P = (500 − 250)·4.021 = 1005 W = 1.005 kW

Answer

P = 1.005 kW
2.Gears & gear trains

Answer: P = 5.918 kW

Belt drives: without slip, both pulleys have the same rim speed v = π·d·n/60, so n₁·d₁ = n₂·d₂ and the speed ratio is d₂/d₁. Slip s makes the driven pulley a little slower: n₂ = n₁·(d₁/d₂)·(1 − s). The power transmitted is P = (T₁ − T₂)·v, with T₁ the tension on the tight side and T₂ on the slack side. Friction limits the ratio of the tensions: T₁/T₂ = eμθ, where θ is the angle of wrap in radians on the smaller pulley; for an open belt θ = π − 2·asin((d₂ − d₁)/(2C)) with centre distance C.

Angle of wrap

θ = 2.933 rad

Slack-side tension

eμθ = e0.7332 = 2.082, T₂ = 1200/2.082 = 576.4 N

Power

P = (1200 − 576.4)·9.49 = 5.918 kW

Answer

P = 5.918 kW
3.Torsion of shafts

Answer: τmax = 63.66 MPa

Torsion of circular shafts: shear stress grows linearly from zero at the centre to τmax = T·r/J at the surface, with J = πd⁴/32 for a solid shaft and J = π(do⁴ − di⁴)/32 for a hollow one. The angle of twist is φ = TL/(GJ) in radians. Power and torque are linked by P = T·ω.

Stress in each segment

T = 100 N·m = 100000 N·mm
τAB = 16·100000/(π·25³) = 32.59 MPa
τBC = 16·100000/(π·20³) = 63.66 MPa

Answer

τmax = 63.66 MPa
4.Torsion of shafts

Answer: τmax = 191 MPa

Torsion of circular shafts: shear stress grows linearly from zero at the centre to τmax = T·r/J at the surface, with J = πd⁴/32 for a solid shaft and J = π(do⁴ − di⁴)/32 for a hollow one. The angle of twist is φ = TL/(GJ) in radians. Power and torque are linked by P = T·ω.

Internal torques

Sense of TC taken as positive.

TBC = TC = 100 N·m
TAB = TC + TB = 100 + 200 = 300 N·m

Maximum shear stress

The segment with the largest internal torque has the largest stress (same diameter).

|T|max = 300 N·m
τmax = 16·300000/(π·20³) = 191 MPa

Answer

τmax = 191 MPa
5.Mohr’s circle & stress transformation

Answer: θp = 37.98 °

Plane stress transformation: on a plane rotated by θ, σ = (σₓ + σᵧ)/2 + (σₓ − σᵧ)/2·cos 2θ + τₓᵧ·sin 2θ. Mohr’s circle shows all planes at once: its centre is at C = (σₓ + σᵧ)/2 and its radius is R = √(((σₓ − σᵧ)/2)² + τₓᵧ²). The principal stresses are C ± R, and the largest in-plane shear stress is R.

σxyCσ1​σ2​

Angle on the circle

Point x sits at an angle 2θp from the σ-axis on Mohr’s circle; the quadrant follows from the signs of σₓ − σᵧ and τₓᵧ.

2θp = atan2(2·20, 80 − 70) = 75.96°

Angle on the element

θp = 37.98°

Answer

θp = 37.98°

Positive angles are counter-clockwise.

6.Mohr’s circle & stress transformation

Answer: σθ = 30.64 MPa

Plane stress transformation: on a plane rotated by θ, σ = (σₓ + σᵧ)/2 + (σₓ − σᵧ)/2·cos 2θ + τₓᵧ·sin 2θ. Mohr’s circle shows all planes at once: its centre is at C = (σₓ + σᵧ)/2 and its radius is R = √(((σₓ − σᵧ)/2)² + τₓᵧ²). The principal stresses are C ± R, and the largest in-plane shear stress is R.

Transformation equation

σθ = 40 + 110·0.342 + −50·0.9397 = 30.64 MPa

Answer

σθ = 30.64 MPa
7.Axial stress & strain

Answer: δ = 24.56 mm

Hooke’s law: within the elastic range σ = E·ε. Combining with σ = P/A and ε = δ/L gives δ = PL/(AE).

Stress

A = π·10²/4 = 78.54 mm²
σ = P/A = 90·1000/78.54 = 1146 MPa

Strain (Hooke’s law)

E for aluminium = 70 GPa = 70000 MPa.

ε = σ/E = 1146/70000 = 0.01637 = 16370 µε

Elongation

δ = ε·L = 0.01637·1500 mm = 24.56 mm

Answer

δ = 24.56 mm
8.Axial stress & strain

Answer: σ2 = 34.33 MPa

Two materials: in series (one after the other) every segment carries the same force and the elongations add: δ = P·Σ L/(E·A). In parallel (side by side between rigid plates) both parts shorten by the same amount, so their strains are equal: the stiffer part takes the larger share, Pi = P·EiAi/ΣEA, and σi = Ei·ε. A bar held between two rigid walls with a load at the junction is statically indeterminate: the two segments share the load in proportion to their stiffness k = EA/L.

Stiffnesses

k₁ = 200000·490.9/400 = 245437 N/mm
k₂ = 100000·1257/200 = 628319 N/mm

Share of segment 2

F2 = 60000·628319/873755 = 43146 N

Stress

σ2 = 43146/1257 = 34.33 MPa (compression)

Answer

σ2 = 34.33 MPa
9.Column buckling

Answer: Pcr = 5.888 kN

Euler buckling: a slender column becomes unstable at Pcr = π²EI/(KL)², where KL is the effective length: K = 1 for pinned–pinned, 2 for fixed–free, 0.7 for fixed–pinned and 0.5 for fixed–fixed. It buckles about the axis with the smallest I. The formula holds for slender columns, whose critical stress stays below the yield stress.

Smallest second moment of area

A round section has the same I about every axis.

I = πd⁴/64 = π·50⁴/64 = 306796 mm⁴

Effective length

KL = 2·3000 = 6000 mm

Critical load

Pcr = π²EI/(KL)² = π²·70000·306796/6000² = 5888 N = 5.888 kN

Answer

Pcr = 5.888 kN
10.Column buckling

Answer: d = 74.06 mm

Euler buckling: a slender column becomes unstable at Pcr = π²EI/(KL)², where KL is the effective length: K = 1 for pinned–pinned, 2 for fixed–free, 0.7 for fixed–pinned and 0.5 for fixed–fixed. It buckles about the axis with the smallest I. The formula holds for slender columns, whose critical stress stays below the yield stress.

Required critical load

Pcr = n·P = 3·85000 = 255000 N
KL = 0.5·4000 = 2000 mm

Solve for the diameter

d = (64·n·P·(KL)²/(π³E))^(1/4) = (64·255000·2000²/(π³·70000))^(1/4) = 74.06 mm

Answer

d = 74.06 mm

Check: the slenderness KL/r is 108, so the column is slender and Euler applies.

11.Mechanical vibrations

Answer: ζ = 0.05997

Free vibration of a mass–spring system: the undamped natural frequency is ωn = √(k/m) in rad/s, and fn = ωn/(2π) in Hz. A viscous damper c gives the damping ratio ζ = c/cc, with critical damping cc = 2·√(k·m) = 2·m·ωn. An underdamped system (ζ < 1) oscillates at ωd = ωn·√(1 − ζ²). Springs in parallel add, k = k₁ + k₂; springs in series add as reciprocals, 1/k = 1/k₁ + 1/k₂.

Logarithmic decrement

δ = (1/2)·ln(10/4.7) = 0.3775

Damping ratio

ζ = δ/√(4π² + δ²) = 0.3775/√(39.48 + 0.1425) = 0.05997

Answer

ζ = 0.05997
12.Mechanical vibrations

Answer: fn = 5.257 Hz

Free vibration of a mass–spring system: the undamped natural frequency is ωn = √(k/m) in rad/s, and fn = ωn/(2π) in Hz. A viscous damper c gives the damping ratio ζ = c/cc, with critical damping cc = 2·√(k·m) = 2·m·ωn. An underdamped system (ζ < 1) oscillates at ωd = ωn·√(1 − ζ²). Springs in parallel add, k = k₁ + k₂; springs in series add as reciprocals, 1/k = 1/k₁ + 1/k₂.

Equivalent stiffness

Only k1 and k2 are in parallel. That pair is in series with k3, so combine them as reciprocals.

k12 = 12 + 12 = 24 kN/m
keq = 24·20/(24 + 20) = 10.91 kN/m

Natural frequency

ωn = √(10909/10) = 33.03 rad/s
fn = 33.03/(2π) = 5.257 Hz

Answer

fn = 5.257 Hz

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